Properties (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turboshaft engine
|
| gptkbp:application |
civil and military aviation
|
| gptkbp:compressionRatio |
16:1
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:design |
modular design
|
| gptkbp:diameter |
0.4 m
|
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:emissionsStandard |
ICAO_Chapter_4
|
| gptkbp:engineType |
free turbine
|
| gptkbp:exhaustSystem |
annular combustion chamber
|
| gptkbp:firstFlight |
1990
|
| gptkbp:fuelType |
gptkb:Jet_A-1
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce 500
|
| gptkbp:launchSite |
electric starter
|
| gptkbp:length |
1.2 m
|
| gptkbp:maintenance |
2000 hours
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Holdings
|
| gptkbp:noise_level |
low noise
|
| gptkbp:operationalStatus |
up to 900 °C
|
| gptkbp:powerOutput |
500 shp
|
| gptkbp:type |
turbo-shaft engine
|
| gptkbp:usedIn |
helicopters
|
| gptkbp:weight |
approximately 150 kg
|